{"created":"2023-06-20T14:36:09.066733+00:00","id":2456,"links":{},"metadata":{"_buckets":{"deposit":"01a05f04-7113-4c79-b967-6adb3ca76ada"},"_deposit":{"created_by":1,"id":"2456","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"2456"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00002456","sets":["1887:1893","9:1090:1114:1124"]},"author_link":["6563","6561","6560","6562","6564","6565"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Uncertainty Analysis of Wind Tunnel Test in the JAXA 2m × 2m Transonic Wind Tunnel"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2016-10-20","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"68","bibliographicPageStart":"1","bibliographicVolumeNumber":"JAXA-RM-16-001","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構研究開発資料"},{"bibliographic_title":"JAXA Research and Development Memorandum","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"JAXA 2m×2m遷音速風洞における風試不確かさ解析用の処理プログラムを開発し、その適用事例としてAGARD-B標準模型を用いた風洞試験に適用した結果について報告する。本プログラムは空力係数の不確かさを各測定量の不確かさから計算する。各測定量の不確かさが空力係数に及ぼす影響度である感度係数の算出は煩雑であるが、本プログラムにより各測定量の不確かさと天秤計測値を入力条件として与えるだけで自動的に感度係数を計算し、空力係数の不確かさを算出できるようになった。なお、本プログラムはJAXAが開発し、平成25年度より運用を開始している「デジタル/アナログ・ハイブリッド風洞（DAHWIN）」の一機能である風試不確かさ解析機能として実装されており、実際の風洞試験に適用されている。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"To estimate uncertainties in the JAXA 2m × 2m transonic wind Tunnel test data, we developed a new uncertainty estimation program and applied it for a wind tunnel test using the AGARD-B calibration model. This program computes uncertainties in aerodynamic coefficients by accumulating uncertainties in measurement data. Computing sensitivity coefficients, which indicate the impact of the uncertainties in the measurement data on the aerodynamic coefficients, is very complicated. This program automatically computes these sensitivity coefficients and evaluates the aerodynamic coefficient uncertainties. This program is implemented in the Digital/Analog Hybrid Wind Tunnel (DAHWIN) developed by JAXA and has been applied for wind tunnel tests since FY2013.","subitem_description_type":"Other"}]},"item_3_description_18":{"attribute_name":"内容記述","attribute_value_mlt":[{"subitem_description":"形態: カラー図版あり","subitem_description_type":"Other"}]},"item_3_description_19":{"attribute_name":"内容記述（英）","attribute_value_mlt":[{"subitem_description":"Physical characteristics: Original contains color illustrations","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA1630022000","subitem_description_type":"Other"}]},"item_3_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: JAXA-RM-16-001","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構(JAXA)"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-1121","subitem_source_identifier_type":"ISSN"}]},"item_3_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA11983593","subitem_source_identifier_type":"NCID"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"宇宙航空研究開発機構航空技術部門空力技術研究ユニット(JAXA)"},{"subitem_text_value":"宇宙航空研究開発機構航空技術部門空力技術研究ユニット(JAXA)"},{"subitem_text_value":"宇宙航空研究開発機構航空技術部門空力技術研究ユニット(JAXA)"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Aerodynamics Research Unit, Aeronautical Technology Directorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Aerodynamics Research Unit, Aeronautical Technology Directorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Aerodynamics Research Unit, Aeronautical Technology Directorate, Japan Aerospace Exploration Agency (JAXA)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"越智, 康浩"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"口石, 茂"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"永井, 伸治"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ochi, Yasuhiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kuchiishi, Shigeru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nagai, Shinji","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2020-01-15"}],"displaytype":"detail","filename":"AA1630022000.pdf","filesize":[{"value":"1.8 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"AA1630022000.pdf","url":"https://jaxa.repo.nii.ac.jp/record/2456/files/AA1630022000.pdf"},"version_id":"c8365f9e-d45e-4839-9fad-d568a6b20987"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Transonic Wind Tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Uncertainty Analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"AGARD-B","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"jpn"}]},"item_resource_type":{"attribute_name":"資源タイプ","attribute_value_mlt":[{"resourcetype":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"JAXA 2m×2m 遷音速風洞における風試不確かさ解析","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"JAXA 2m×2m 遷音速風洞における風試不確かさ解析"}]},"item_type_id":"3","owner":"1","path":["1124","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2016-10-20"},"publish_date":"2016-10-20","publish_status":"0","recid":"2456","relation_version_is_last":true,"title":["JAXA 2m×2m 遷音速風洞における風試不確かさ解析"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T09:22:26.537447+00:00"}